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[ANSYS Meshing] Icem generated mesh changing in cfx solver

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Old   April 28, 2016, 21:09
Default Icem generated mesh changing in cfx solver
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Faizan
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Hi all,

I am facing problems in convergence for a steady state flow on CFX. I am simulating a supersonic flow using deLaval nozzle. I have three domains. 1. Surrounding air Fluid Domain. 2. Solid Nozzle domain and 3. High pressure Nitrogen Fluid Domain. I built the mesh on ICEM in an assembled form then I exported all three domains separately. I imported three domains in CFX and used GGI interface for wall connection for all three domains. It is surprising that CFX Solver changed the mesh quality which I built in ICEM. The ortho, aspect ratio and exp.factor values were changed by solver.

The simulation is failing when at a point when high pressure nitrogen mixes with surrounding air. I am posting a pictures of existing mesh. Please suggest how can I overcome this mesh problem. I don't want to increase the mesh elements. I need guidance to increase the mesh quality for supersonic flow to achieve convergence.

Any help/suggestion would be appreciated.

thanks in advance,

regards,

Faizan
Attached Images
File Type: jpg Area away from nozzle exit.jpg (204.2 KB, 5 views)
File Type: jpg Nozzle Exit-Mixing with cylinder surrounding air domain mesh.jpg (201.7 KB, 3 views)
File Type: jpg Nozzle Throat.jpg (201.3 KB, 4 views)
File Type: jpg Overall Mesh Region.jpg (191.3 KB, 4 views)
File Type: jpg Overall Mesh.jpg (197.6 KB, 2 views)
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Old   April 28, 2016, 21:11
Default more pics attached
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More pics attached
Attached Images
File Type: jpg Overall x sec mesh.jpg (205.4 KB, 0 views)
File Type: jpg overall x section away form nozzle exit.jpg (205.1 KB, 0 views)
File Type: jpg Region close to nozzle convergent section.jpg (201.1 KB, 0 views)
File Type: jpg x section around nozzle.jpg (183.8 KB, 1 views)
File Type: jpg x section at throat Big Mesh.jpg (201.3 KB, 1 views)
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Old   April 28, 2016, 21:12
Default more pics
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more pics of mesh
Attached Images
File Type: jpg x section at throat.jpg (199.2 KB, 2 views)
File Type: jpg x section away from nozzle exit in surrounding domain.jpg (203.3 KB, 1 views)
File Type: jpg xsec more away from nozzle exit.jpg (198.9 KB, 2 views)
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Old   April 29, 2016, 09:40
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The mesh jumps to brute from one to the another.
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Old   May 1, 2016, 22:36
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Hi Dr.Flow,

Yes- I agree with you. I am new to ICEM meshing. I used Bigeometric rule with 1.2 edge ratio. Now I would appreciate if you can assist me to develop a quality mesh for three domains without increasing mesh density. Any coarse mesh with high quality would be sufficient for my project because I need to expedite the convergence.

Thanks

Faizan.
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Old   May 2, 2016, 04:35
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Hi all,

Please advice/suggest me as what should I do to incerase the quality of mesh on icem. I am new to ICEM and do not know much option. I am using bigeomteric rule under edge parameter. I linked the spacing with 1.2. I once increased the no. of nodes but it only increased the solver time. No significant change.

As I mentioned earlier that when I import the mesh in cfx using workbench. I used GGI interface option and cfx automatically oriented the nodes for two fluid domains and once solid domains. It is changing the mesh ortho, aspet ration but not the exp factor.

I was on other forum and a gyu told me to go to icem forum to fix the expansion ratio issue.

Please help...any expert opinion will be highly appreciated.

Thanks
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Old   May 2, 2016, 04:37
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how to handle the expansion ration on ICEM???
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